Path: Orbit/Optimization

% Demonstrate the 2D trajectory optimization function for low thrust.
 This demo is the same as the built-in demo in TrajectoryOptimization, a
 low-thrust transfer to Mars. This is a well-studied problem. The method used
 is downhill simplex.

 Things to try: see how the methods do with different initial costates. 

 See also Constant, Planets, TrajectoryOptimization


Orbit: Optimization/CostLowThrust2D
Orbit: Optimization/FLowThrust2D
Orbit: Optimization/Plot2DTrajectory
Orbit: Optimization/TrajectoryOptimization
SC: BasicOrbit/VOrbit
SC: Ephem/Planets
Common: Database/Constant

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